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EN 2.4650 Nickel vs. 319.0 Aluminum

EN 2.4650 nickel belongs to the nickel alloys classification, while 319.0 aluminum belongs to the aluminum alloys. There are 30 material properties with values for both materials. Properties with values for just one material (2, in this case) are not shown. Please note that the two materials have significantly dissimilar densities. This means that additional care is required when interpreting the data, because some material properties are based on units of mass, while others are based on units of area or volume.

For each property being compared, the top bar is EN 2.4650 nickel and the bottom bar is 319.0 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 210
72
Elongation at Break, % 34
1.8 to 2.0
Fatigue Strength, MPa 480
76 to 80
Poisson's Ratio 0.29
0.33
Shear Modulus, GPa 80
27
Shear Strength, MPa 730
170 to 210
Tensile Strength: Ultimate (UTS), MPa 1090
190 to 240
Tensile Strength: Yield (Proof), MPa 650
110 to 180

Thermal Properties

Latent Heat of Fusion, J/g 320
480
Maximum Temperature: Mechanical, °C 1010
170
Melting Completion (Liquidus), °C 1400
600
Melting Onset (Solidus), °C 1350
540
Specific Heat Capacity, J/kg-K 450
880
Thermal Conductivity, W/m-K 12
110
Thermal Expansion, µm/m-K 11
22

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 1.5
27
Electrical Conductivity: Equal Weight (Specific), % IACS 1.6
84

Otherwise Unclassified Properties

Base Metal Price, % relative 80
10
Density, g/cm3 8.5
2.9
Embodied Carbon, kg CO2/kg material 10
7.7
Embodied Energy, MJ/kg 140
140
Embodied Water, L/kg 360
1080

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 320
3.3 to 3.9
Resilience: Unit (Modulus of Resilience), kJ/m3 1030
88 to 220
Stiffness to Weight: Axial, points 13
14
Stiffness to Weight: Bending, points 23
48
Strength to Weight: Axial, points 36
18 to 24
Strength to Weight: Bending, points 28
25 to 30
Thermal Diffusivity, mm2/s 3.1
44
Thermal Shock Resistance, points 33
8.6 to 11

Alloy Composition

Aluminum (Al), % 0.3 to 0.6
85.8 to 91.5
Boron (B), % 0 to 0.0050
0
Carbon (C), % 0.040 to 0.080
0
Chromium (Cr), % 19 to 21
0
Cobalt (Co), % 19 to 21
0
Copper (Cu), % 0 to 0.2
3.0 to 4.0
Iron (Fe), % 0 to 0.7
0 to 1.0
Magnesium (Mg), % 0
0 to 0.1
Manganese (Mn), % 0 to 0.6
0 to 0.5
Molybdenum (Mo), % 5.6 to 6.1
0
Nickel (Ni), % 46.9 to 54.2
0 to 0.35
Phosphorus (P), % 0 to 0.020
0
Silicon (Si), % 0 to 0.4
5.5 to 6.5
Sulfur (S), % 0 to 0.0070
0
Titanium (Ti), % 1.9 to 2.4
0 to 0.25
Zinc (Zn), % 0
0 to 1.0
Residuals, % 0
0 to 0.5